Invention Grant
US08771786B2 Method for repair of a component of a turbomachine and a component repaired according to this method 有权
根据该方法修复涡轮机组件和修理部件的方法

Method for repair of a component of a turbomachine and a component repaired according to this method
Abstract:
A method is disclosed for the repair of a component of a turbomachine, in particular a rotor of an aircraft gas turbine, with blades taken up in at least one groove and with at least one support region for limiting a blade tilt angle, whereby at least one segment, which has been subjected to wear, of the support region of the component is removed, and a coating that can be introduced in the unit on at least one supporting surface of at least one blade is formed on the component for limiting the blade tilt angle. In addition, a component of a turbomachine, in particular a rotor of an aircraft gas turbine, with at least one such repair site is disclosed.
Information query
Patent Agency Ranking
0/0